A new active and passive asynchronous fusion tracking of maneuvering target - art. no. 63585H

被引:0
作者
Wei, Zhang [1 ]
Hong, Jiang [1 ]
Long, Song [1 ]
Zhang, Ren [1 ]
机构
[1] Beihang Univ, Sch Automat, Beijing 100083, Peoples R China
来源
Sensors, Automatic Measurement, Control, and Computer Simulation, Pts 1 and 2 | 2006年 / 6358卷
关键词
data fusion; delicate time-slicing; feedback fusion; active target tracking (ATT); passive target tracking (PTT); Converted Measurement Kalman Filter (CMKF); Pseudo Linear Estimator (PLE) with frequency information;
D O I
10.1117/12.718385
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A new asynchronous data fusion algorithm was adopted in this paper. This new fusion algorithm was based on the feedback fusion and the delicate time-slicing. Its basic idea is: at instants with neither passive (PTT) nor active target tracking (ATT) measurements, it will predict this instant's states based on last instant's filtering result; at instants with only active or passive target tracking measurement, it will use its own filtering algorithm i.e., Converted Measurement Kalma-n Filter (CMKF) for active radar, Pseudo Linear Estimator (PLE) with frequency information for passive radar to get this instant's states; at instants with both passive and active target tracking measurements, it will fuse the active and passive measurements by feedback fusion algorithm, with the passive radar receiving the feedback information. The advantage of this new algorithm is that it can fuse the active and passive target tracking with non multiple integer sampling period ratio. This paper also extended the 2D constant velocity moving target to the 3D maneuvering target. Simulation results indicate that the new fusion algorithm can improve the tracking performance in some acceptable degree.
引用
收藏
页码:H3585 / H3585
页数:5
相关论文
共 6 条
  • [1] HE Y, 2000, ACTA ELECT SINICA, V28
  • [2] HE Y, 2003, J AERONAUTICS, V24
  • [3] XIN G, 2003, J SYSTEM SIMULATION, V15
  • [4] XIU JJ, 2001, SYSTEMS ENG ELECT, V23
  • [5] XU YW, 1998, J NATL U DEFENSE TEC, V20
  • [6] ZHANG XG, 2001, AERONAUTICAL COMPUTE, V31